Implicit LES of compressible turbulent flow over a backward-facing step

Keiichi Ishiko, Kazuyuki Ueno, Keisuke Sawada

Research output: Contribution to journalConference articlepeer-review

Abstract

An implicit LES code utilizing the Weighted Compact Nonlinear Scheme is developed. A shock diffraction problem and the boundary layer flow over a flat plate are solved to examine the applicability of the developed code for compressible turbulent flowfleld. A supersonic flowfleld over a backward-facing step both in two- and three-dimensional space is then solved. It is shown that characteristic features of the flowfleld are well captured in the computed results. However, a quantitative agreement of the surface pressure profile along the centerline with that of the experimental data is yet to be accomplished. Possible causes are examined.

Original languageEnglish
Article number2008-6579
JournalCollection of Technical Papers - AIAA Applied Aerodynamics Conference
DOIs
Publication statusPublished - 2008 Jan 1
Event26th AIAA Applied Aerodynamics Conference - Honolulu, HI, United States
Duration: 2008 Aug 182008 Aug 21

ASJC Scopus subject areas

  • Engineering(all)

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